FR3099134B1 - Procédé d’alimentation électrique d’un réseau électrique et architecture électrique - Google Patents

Procédé d’alimentation électrique d’un réseau électrique et architecture électrique Download PDF

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Publication number
FR3099134B1
FR3099134B1 FR1908442A FR1908442A FR3099134B1 FR 3099134 B1 FR3099134 B1 FR 3099134B1 FR 1908442 A FR1908442 A FR 1908442A FR 1908442 A FR1908442 A FR 1908442A FR 3099134 B1 FR3099134 B1 FR 3099134B1
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FR
France
Prior art keywords
electrical
electric
network
power supply
main
Prior art date
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Application number
FR1908442A
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English (en)
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FR3099134A1 (fr
Inventor
Marc Gazzino
Christophe Mouton
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters SAS
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Airbus Helicopters SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Helicopters SAS filed Critical Airbus Helicopters SAS
Priority to FR1908442A priority Critical patent/FR3099134B1/fr
Priority to EP20180283.2A priority patent/EP3771059A1/fr
Priority to US16/903,580 priority patent/US11554875B2/en
Publication of FR3099134A1 publication Critical patent/FR3099134A1/fr
Application granted granted Critical
Publication of FR3099134B1 publication Critical patent/FR3099134B1/fr
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Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J1/00—Circuit arrangements for dc mains or dc distribution networks
    • H02J1/10—Parallel operation of dc sources
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05F—SYSTEMS FOR REGULATING ELECTRIC OR MAGNETIC VARIABLES
    • G05F1/00—Automatic systems in which deviations of an electric quantity from one or more predetermined values are detected at the output of the system and fed back to a device within the system to restore the detected quantity to its predetermined value or values, i.e. retroactive systems
    • G05F1/10—Regulating voltage or current
    • G05F1/625—Regulating voltage or current wherein it is irrelevant whether the variable actually regulated is ac or dc
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
    • H02J7/16—Regulation of the charging current or voltage by variation of field
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

La présente invention concerne un procédé d’alimentation électrique d’un réseau électrique non régulé en tension électrique ainsi qu’une architecture électrique (5). Ladite architecture électrique (5) comporte plusieurs sources d’énergie électrique (11,19) dont au moins un dispositif de stockage d’énergie électrique rechargeable (52) et un générateur électrique (51), un réseau électrique principal (20) relié directement électriquement auxdites sources d’énergie électrique (11,19) et des équipements électriques (13) alimentés électriquement par ledit réseau électrique principal (20). Ledit procédé comporte une première alimentation électrique (110) dudit réseau électrique principal (20) par ledit dispositif de stockage d’énergie électrique rechargeable (52), et une seconde alimentation électrique (120) dudit réseau électrique principal (20) par ledit générateur électrique (51), puis une régulation (130) d’une tension électrique interne dudit générateur électrique (51) en fonction d’un premier courant électrique délivré par ledit dispositif de stockage d’énergie électrique rechargeable (52). Figure abrégé : figure 1
FR1908442A 2019-07-25 2019-07-25 Procédé d’alimentation électrique d’un réseau électrique et architecture électrique Active FR3099134B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1908442A FR3099134B1 (fr) 2019-07-25 2019-07-25 Procédé d’alimentation électrique d’un réseau électrique et architecture électrique
EP20180283.2A EP3771059A1 (fr) 2019-07-25 2020-06-16 Procédé d'alimentation électrique d'un réseau électrique et architecture électrique
US16/903,580 US11554875B2 (en) 2019-07-25 2020-06-17 Method of electrically powering an electricity network, and an electrical architecture

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1908442 2019-07-25
FR1908442A FR3099134B1 (fr) 2019-07-25 2019-07-25 Procédé d’alimentation électrique d’un réseau électrique et architecture électrique

Publications (2)

Publication Number Publication Date
FR3099134A1 FR3099134A1 (fr) 2021-01-29
FR3099134B1 true FR3099134B1 (fr) 2021-10-15

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
FR1908442A Active FR3099134B1 (fr) 2019-07-25 2019-07-25 Procédé d’alimentation électrique d’un réseau électrique et architecture électrique

Country Status (3)

Country Link
US (1) US11554875B2 (fr)
EP (1) EP3771059A1 (fr)
FR (1) FR3099134B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3130253A1 (fr) * 2021-12-09 2023-06-16 Airbus Helicopters Installation motrice pour aéronef, aéronef et procédé de fonctionnement d’une telle installation
JP2023147339A (ja) * 2022-03-30 2023-10-13 本田技研工業株式会社 航空機の制御装置
SE545936C2 (en) * 2022-07-29 2024-03-19 Heart Aerospace AB An energy distribution system

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08205312A (ja) * 1995-01-19 1996-08-09 Nippondenso Co Ltd シリーズハイブリッド車の制御方法及びその制御装置
US6091228A (en) * 1998-04-29 2000-07-18 Lockheed Martin Corp. Control system for, in the presence of a varying system load, establishing generator current to maintain a particular battery charge state
US7075273B2 (en) * 2004-08-24 2006-07-11 Motorola, Inc. Automotive electrical system configuration using a two bus structure
JP4595933B2 (ja) * 2006-12-12 2010-12-08 株式会社デンソー 車両用バッテリ電流検出装置
DE102007055336A1 (de) * 2007-01-15 2008-08-21 GIF Gesellschaft für Industrieforschung mbH Flugzeugpropellerantrieb, Verfahren zum Antreiben eines Flugzeugpropellers und Verwendung eines Lagers eines Flugzeugpropellerantriebs sowie Verwendung einer Elektromaschine
FR3056555B1 (fr) 2016-09-29 2018-12-07 Safran Helicopter Engines Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac
US10233768B1 (en) * 2018-03-22 2019-03-19 Florida Turbine Technologies, Inc. Apparatus and process for optimizing turbine engine performance via load control through a power control module
US10759545B2 (en) * 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
EP3772462A1 (fr) * 2019-08-05 2021-02-10 Hamilton Sundstrand Corporation Régénération d'énergie d'aéronef électrique hybride

Also Published As

Publication number Publication date
US20210024223A1 (en) 2021-01-28
EP3771059A1 (fr) 2021-01-27
US11554875B2 (en) 2023-01-17
FR3099134A1 (fr) 2021-01-29

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